Airbus A320-211

Service difficulty reports · 5,271

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duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = 'A320211'
  ORDER BY difficulty_date DESC"

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SDR DALA2016111808972Dummy Rail · corrodedCORROSION ON DUMMY RAIL BETWEEN FRAMES 12 TO 16. REPLACED THE DUMMY RAIL IAW SRM.Oct 23, 2015 · N325US · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015102406413Stringer · corrodedCORROSION ON SECTION CONNECTION ON STR 29LT INTERNAL STRUCTURE LEVEL FRAME 67 AT LOWER FUSELAGE. REPLACED SECTION CONNECTION AND FASTENERS ON STR 29LT INTERNAL STRUCTURE LEVEL FRAME 67 AT LOWER FUSELAGE IAW SRM 51-72-11 AND DWG D53480019.Oct 23, 2015 · N325US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA2015102406412Seat Track · corrodedOUT OF LIMITS, SEAT TRACK +Y1292 ON CENTER WING BOX BETWEEN FRAME 41 TO FRAME 47. MEASURE OF REWORK ARE L: 2.722", W: 0.374", D: 0.096", REPLACED SEAT TRACK +Y1292 ON CENTER WING BOX BETWEEN FRAME 41 TO FRAME 47 IAW SRM 51-72-11 AND DWG D53370500 AND D533710Oct 23, 2015 · N325US · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015102306407Floor Support · corrodedCORROSION ON FLOORBEAM -Y1292 LOCATED FRAME 12 TO FRAME 24 MEASURE ARE L=0, 250" W=0.125", D=O.010", APPROXIMATELY SSI 531189 AT FWD GALLEY AREA. REPLACED FLOORBEAM Y1292 LOCATED FRAME 12 TO FRAME 24 IAW SRM 51-72-11 AND DWG D53112812.Oct 22, 2015 · N325US · Airbus A320211 · Fuselage Miscellaneous StructureSDR CA151021002Valve · leaking(CAN) AFTER DEPARTURE, CREW UNABLE TO RETRACT ALL GEAR. NOISE HEARD FROM MAIN LANDING GEAR. AIRCRAFT DIVERTING BACK TO DEPARTURE AIRPORT AFTER BURNING OFF FUEL DUE MAX LANDING WEIGHT COMPROMISED. RESOLUTION FOUND DAMAGED, LEAKING SEAL AT NLG SHOCK ABSORBER PROct 20, 2015 · Airbus A320211 · Nose/Tail Landing Gear Strut/AxleSDR DALA2015101906244Floor Support · corrodedCORROSION ON FLOOR SUPPORT -Y1162 BETWEEN FRAMES 67+15 - 69. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D5347200.Oct 18, 2015 · N325US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2015101906243Floor Support · corrodedCORROSION ON FLOOR SUPPORT +Y1162 BETWEEN FRAMES 67+15 - 69. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.Oct 18, 2015 · N325US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2015101906242Floor Support · corrodedCORROSION ON FLOOR SUPPORT +Y1225 BETWEEN FRAMES 66+5 - 67+15. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.Oct 18, 2015 · N325US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2015101606218Fitting · corrodedCORROSION ON CORNER FITTING FRAME 68 AT LEVEL STR 23L AT AFT GALLEY AREA. REPLACED CORNER FITTING LOCATED FRAME 68 AT LEVEL STR 23L AFT GALLEY AREA IAW SRM 51-72-11 AND DWG D53480020.Oct 15, 2015 · N325US · Airbus A320211 · Fuselage Miscellaneous StructureSDR CA151013003Engine · malfunctioned(CAN) AIRBORNE RETURN TO DEPARTURE AIRPORT SHORTLY AFTER TAKEOFF DUE TO A MECHANICAL ISSUE WITH EGT EXCEEDED. ENGINE NR 1 REPLACED IAW TASK CARD 2-271A-01.Oct 12, 2015 · Airbus A320211 · Engine (Turbine/Turboprop)SDR CA151013013Connector · contaminated(CAN) REJECTED TAKEOFF AT 70KTS DUE TO ECAM ENGINE 1 REVERSER UNLOCKED DURING TAKEOFF ROLL. MAX BRAKE TEMP AFTER STOP WAS BRAKE-4 AT 445 DEGREE C, NON DISPATCHABLE FAULT. WILL GO TO HANGAR FOR TSID. T/S 78-31-00-810-839 CARRIED OUT. FOUND BLOCKER DOOR STOWOct 11, 2015 · Airbus A320211 · Engine Exhaust System WiringSDR CA151013002Support · loose(CAN) AFTER TAKEOFF FLIGHT INCURRED A LANDING GEAR SHOCK ABSORBER FAULT AND AN INDICATION THAT THE NOSE WHEEL DOORS WERE NOT CLOSED AND LOCKED. A PATCH WITH MAINTENANCE CONTROL WAS CARRIED OUT. THE PILOT DID NOT WANT TO RETURN OUT OF CONCERNS FOR POSSIBLE TUOct 10, 2015 · Airbus A320211 · Landing Gear Position and WarningSDR DALA2015100805994Spar · wornWEAR ON BOTTON SKIN REINFORCING PLATE REAR SPAR ON RT WING FROM RIB 7 TO RIB 8. REPLACED REINFORCING PLATE REAR SPAR ON RT WING FROM RIB 7 TO RIB 8 IAW SRM 57-21-11 PARA 5.E, FIG 205.Oct 7, 2015 · N326US · Airbus A320211 · Wing SparSDR DALA2015100805993Spar · wornWEAR ON BOTTON SKIN REIFORCING PLATE REAR SPAR ON LT WING FROM RIB 7 TO RIB 8. REPLACED REINFORCING PLATE REAR SPAR ON LT WING FROM RIB 7 TO RIB 8 IAW SRM 57-21-11, PARA 5.E, FIG 205.Oct 7, 2015 · N326US · Airbus A320211 · Wing SparSDR DALA2015100705986Skin · damagedMISSING MATERIAL ON SLAT 3 INBD EDGE AT T/E AREA ON RT WING. PERFORMED REPAIR ON SLAT 3 INBD EDGE AT T/E AREA ON RT WING IAW PRI ER/A 539117-14, REV 0 AND ER/A 539117-14.Oct 7, 2015 · N326US · Airbus A320211 · Leading Edge DevicesSDR DALA2015100705987Power Supply · inoperativeNUMEROUS EMERGENCY LIGHTS INOPERATIVE ON AISLE SEATS. FOUND AFT UNIT PWR SUPPLY AT FAULT. R & R POWER SUPPLY.Oct 5, 2015 · N319US · Airbus A320211 · Emergency LightingSDR CA151008004Sensor · corroded(CAN) ON ROUTE THE CREW EXPERIENCED MULTIPLE ECAM MESSAGES INCLUDING, A/T OFF, AP1+2 OFF, L/G RETRACT AND CAT2. MAINTENANCE WAS CONSULTED AND THE FLIGHT CONTINUED TO DESTINATION AND LANDED WITHOUT FURTHER INCIDENT. RESOLUTION REPLACED PROXIMITY SENSOR 24GA AOct 4, 2015 · Airbus A320211 · Landing Gear Position and WarningSDR CA150930010Turbine Wheel · corroded(CAN) AFTER INSPECTION OF DISK LPT STG 2,CORROSION IN CRITICAL AREA, TRANSITION RADIUS, HAS BEEN FOUND. ACCORDING TO ATA :72-54-03-200-001 CORROSION IS NOT ALLOWED. IN ADDITION, DAMAGE ON SURFACE "G", DEPTH:0,3 MM, LENGTH:2,58 MM, IS OVER LIMIT ACCORDING TO Sep 28, 2015 · Airbus A320211 · Turbine SectionSDR DALA2015092905867Light · damagedEMERGENCY SEAT MOUNTED LIGHT DAMAGED. REPLACED LIGHT ASSY.Sep 28, 2015 · N313US · Airbus A320211 · Emergency LightingSDR CA150923012Selector · locked(CAN) ON TAXI FOR DEPARTURE, THE ACFT BRAKES LOCKED UP AND WOULD NOT RELEASE. RESOLUTION FOUND PARKING BRAKE SELECTOR VALVE DOES NOT WORK ON NORMAL BRAKE, ONLY ON ALTERNATE. REPLACED SELECTOR VALVE IAW AMM 32-45-51.Sep 22, 2015 · Airbus A320211 · Landing Gear Brake SystemSDR DALA2015092105774Fitting · corrodedCORROSION ON CORNER FITTING FRAME 20 AT FWD GALLEY AREA ON STRINGER 23R, L=0.787", W=0.567", D=0.003", SSI 531102. REPLACED CORNER FITTING LOCATION FRAME 20 AT LEVEL STR 23R FWD GALLEY AREA IAW SRM 51-72-11 AND DWG NR D53112225, REPAIRED IS CLASSIFIED AS MAJOSep 21, 2015 · N334NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2015092205775Light · inoperativeDURING SERVICE CHECK, INTERNAL LOADS EMERGENCY LIGHT FAULTED ON CIDS PANEL ON EMERGENCY LIGHT SYSTEM CHECK. REPAIRED LIGHT AND ALL TESTS OK.Sep 19, 2015 · N316US · Airbus A320211 · Emergency LightingSDR CA150917001Switch · faulted(CAN) PTU ECAM THEN HYD G RESVOIR LOW LEVEL IN CRUIZE. ECAM FOLLOWED. FAULT LT ON HYD PUMP 1 & PTU PB-SWS. HYD G, B, Y, RESVOIR LOW LEVEL ALERT.Sep 15, 2015 · Airbus A320211 · Hydraulic Indicating SystemSDR DALA2019022601219Fitting · crackedAFT CARGO DOOR HANDLE FITTING WAS FOUND CRACKED, TIME LIMITED REPAIR ON DOOR INNER SKIN IN AFT CARGO COMPARTMENT BTW BEAM 4 TO BEAM 5 AND BTW FR 55A TO FR 56 IAW PRI 538027-14 REV. 0,1,2 AND 3 AND ERA 538027-14 REV. ASep 11, 2015 · N317US · Airbus A320211 · Cargo/Baggage DoorsSDR DALA2015091005572Skin · damagedEVIDENCE OF DAMAGE TO LOWER FWD SKIN BETWEEN FRAMES 25-26 AND STRINGERS 44-43R PRI/ERA ISSUED 539169-14 REV 0 REV 1 REV 2 REV 3. C/W PRI/ERA 539169-14 REV 0,1,2 AND 3.Sep 9, 2015 · N322US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA2015090205390Skin · damagedNICK ON EXTERNAL SKIN AT LOWER FUSELAGE ON FRAME 23+4" BETWEEN STRINGER 42L TO STRINGER 43L. PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN AT LOWER FUSELAGE ON FR23+4" BETWEEN STR 42L TO STR 43L IAW SRM 53-00-11, PARA 4W, FIG 238.Sep 1, 2015 · N317US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA2015090105389Feeder Cable · disconnectedEMERGENCY LIGHT INOPERATIVE AT SEAT ROW 8 ABC. CONNECTED FEEDER WIRES AT SEAT DISCONNECT. OPS NORMAL.Aug 31, 2015 · N331NW · Airbus A320211 · Light System WiringSDR DALA2015090105385Stringer · corrodedCORROSION FOUND ON STRINGER 25R BETWEEN FRAMES 64 - 67 . REPLACED THE STRINGER IAW SRM 51-72-11 AND DWG D53480020.Aug 31, 2015 · N317US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR CA150831004Control Unit · failed(CAN) ENGINE 1 THRUST LEVER DISAGREE. ENGINE 1 BROUGHT TO FLIGHT IDLE FOR THE DESCENT AND LANDING. PASSENGERS ADVISED AND NO NEGATIVE REACTION. RESOLUTION THROTTLE CONTROL UNIT REPLACED IAW AMM 76-11-19-060-040A AND AMM 76-11-19-400-040A. AFTER TSM C/O 76-1Aug 30, 2015 · Airbus A320211 · Power LeverSDR CA150826002Fire Detector · failed(CAN) AFTER DEPARTURE WITH ENGINE 1 LOOP B ON MEL, LOOP A ON ENGINE 1 FAILED AND CREW ELECTED RETURN TO DEPARTURE AIRPORT.Aug 26, 2015 · Airbus A320211 · Fire DetectionSDR DALA2015082705380Structure · damagedTHE LT HORIZONTAL STAB L/E WAS DAMAGED IN A HAILSTORM. REPAIRED THE LT L/E.Aug 26, 2015 · N332NW · Airbus A320211 · Horizontal Stabilizer StructureSDR CA150821006Hose · leaking(CAN) ON TAXI OUT FOR DEPARTURE, THE GREEN HYD SYS DEVELOPED A LEAK. HYD FLUID WAS SPILLED ONTO THE TAXI WAY. THE ACFT NEEDED TO BE TOWED BACK TO THE GATE. RESOLUTION NEW BRAKE LINE INSTALLED IAW MM 29-00-00 BRAKE BLED IAW MM 32-42-00 EDP CASE DRAIN FILTER CAug 21, 2015 · Airbus A320211 · Hydraulic System, MainSDR DALA2015081505002Skin · dentedTHE NR 4 RT SLAT WAS FOUND DENTED ALONG THE L/E.Aug 14, 2015 · N332NW · Airbus A320211 · Leading Edge DevicesSDR CA150805007Controller · failed(CAN) AFTER T/O, UNABLE TO PRESSURIZE ACFT, RETURN, SUBSEQUENT OVERWEIGHT LANDING. RESOLUTION POST FLIGHT REPORT SHOWED, NO CPC 1 ANALOG SIGNAL. ON GROUND UNABLE TO FAULT SYS 1, 2 OR MANUAL CONTROL. REPLACED CPC NR 1 IAW AMM 21-31-34 PB401 AND OPS TEST OF TAug 5, 2015 · Airbus A320211 · Cabin Pressure ControllerSDR CA150731005Gcu · failed(CAN) AFTER TAKEOFF ACFT HAD NR 1 GENERATOR ISSUES, FLIGHT RETURNED TO DEPARTURE. RESOLUTION REF TSM 24-00-00-810-805-A, GCU 1 REPLACED IAW AMM 24-22-34 PB401.Jul 31, 2015 · Airbus A320211 · AC RegulatorSDR DALA2015072304609Battery Pack · failedRT SLIDE BATTERY PACK FAILES TEST. REPLACED RT EPSU AND BTTERY PACK AND FUNCTIONAL CHECK WAS NORMAL.Jul 22, 2015 · N309US · Airbus A320211 · Escape SlideSDR DALA2015072304611Power Supply · faultedAFT LT EPSU HAS UNIT FAULT. REPLACED AFT LT EPSU/BATTERY AND OPS CHECK WAS NORMAL.Jul 21, 2015 · N319US · Airbus A320211 · Emergency LightingSDR CA150715001Pump · failed(CAN) AFTER DEPARTURE GREEN HYD SYS FAILED. RETURNED FOR MX. PAN PAN DECLARED WITH ATC. CRASH FIRE RESCUE ON STANDBY FOR ARRIVAL. TOWED TO GATE. AFTER ARRIVAL RESOLUTION CHAFED HYD LINE REPLACED AS PP 320-54-57635. CASE DRAIN, LP & HP HYD FILTERS & EDP RJul 14, 2015 · Airbus A320211 · Hydraulic Pump (Electric/Engine), MainSDR DALA2015071404360Light · inoperativeEMERGENCY LIGHT AT ROW 5 ABC FOUND INOPERATIVE. REPLACED THE EMERGENCY LIGHT AND FUNCTIONAL CHECKED NORMAL.Jul 13, 2015 · N377NW · Airbus A320211 · Emergency LightingSDR DALA2015070904193Power Supply · inoperativeFOUND EMERGENCY LIGHT TEST WOULD NOT PASS. REPLACED THE POWER SUPPLY AND FUNCTIONAL CHECKED NORMAL.Jul 8, 2015 · N327NW · Airbus A320211 · Emergency LightingSDR CA150706002Check Valve · leaking(CAN) HYD ENGINE 2 Y PRESSURE LOW FOLLOWED BY LOSS OF ALL FLUID. ECAM CARRIED OUT. NOTIFIED MAINTENANCE AND CARRIED ON TO DESTINATION. MAJOR LEAK FOUND ON THE PTU MANIFOLD CHECK VALVE, 3094GM, SEALS. CHECK VALVE REPLACED AS OER AMM 29-13-15 PB401.Jul 3, 2015 · Airbus A320211 · Hydraulic System, MainSDR DALA2015062903982Battery Pack · inoperativeDURING EMERGENCY LIGHTS SYSTEM TEST FOUND RT EPSU BATTERY FOUND RT BATTERY INOPERATIVE. REPLACED BATTERY PACK AND FUNCTIONAL CHECK WAS NORMAL.Jun 28, 2015 · N324US · Airbus A320211 · Emergency LightingSDR CA150629017O-Ring · failed(CAN) APPROX 20 MINS OUT CREW HAD A YELLOW HYD FAILURE & DECLARED A PAN PAN WITH ATC NO CFR TRUCKS WERE REQUESTED. ACFT LANDED WITHOUT INCIDENT & WAS ABLE TO TAXI & BRAKE WITHOUT A TOW TO GATE. RESOLUTION CREW SELECTED EDP OFF, YELLOW SYS WAS NOT EMPTY ON ARJun 27, 2015 · Airbus A320211 · Hydraulic System, MainSDR DALA2015062903981Light · damagedEMERGENCY SEAT MOUNTED LIGHTING DAMAGED AND IS INOPERATIVE AT LOCATIONS 4C. REPAIRED LIGHT AND FUNCTIONAL CHECKED NORMAL.Jun 26, 2015 · N320US · Airbus A320211 · Emergency LightingSDR DALA2015061703823Battery Pack · inoperativeFORWARD LT EMERGENCY LIGHT BATTERY PACK IS INOPERATIVE. REPLACED THE BATTERY PACK AND FUNCTIONAL CHECKED NORMAL.Jun 16, 2015 · N317US · Airbus A320211 · Emergency LightingSDR CA150615020Connector · disconnected(CAN) DID A MISSED APPROACH TO RUNWAY DUE TO THE FLAPS NOT EXTENDING. THEY DECLARED A PAN PAN & DID A FLAPLESS LANDING WITHOUT FURTHER INCIDENT. RESOLUTION FOUND CONNECTOR 4035VC-A DISCONNECTED & 4037VC-A NOT CONNECTED PROPERLY. BOTH CONNECTORS RECONNECTEDJun 15, 2015 · Airbus A320211 · Flight Control System WiringSDR CA150601001Gcu · failed(CAN) AFTER DEPARTURE, THE ACFT ENCOUNTERED A DMC 3, FAILURE INFLIGHT. THE FLIGHT CREW ELECTED TO RETURN, THE LANDING WAS NOT OVERWEIGHT & DID NOT REQUIRE ANY DECLARATION OF AN EMERGENCY. THE ACFT WAS MET BY MX & TAKEN OFFLINE FOR TROUBLESHOOTING. DUE FAULTMay 31, 2015 · Airbus A320211 · DC Generating SystemSDR DALA2015052003383Floorbeam · corrodedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM, Y503.2 AT LEVEL OF FR 16 AT FWD GALLEY AREAL=8", W=4", D=0.004". SSI 531189. REPLACED FLOORBEAM Y503.2 AT LEVEL OF FRAME 16 AT FWD GALLEY AREA IAW SRM 51-72-11 AND DWG D53112825.May 19, 2015 · N353NW · Airbus A320211 · Fuselage Main, Floor BeamSDR DALA2016112109086Stringer · damagedDURING INSPECTION, FOUND STRINGER 42R DAMAGED. REMOVED AND REPLACED THE STRINGER IAW ER/A.May 17, 2015 · N332NW · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA2016112109085Stringer · corrodedSTRINGER 43R HAS CORROSION AT FRAMES 25 TO 26. REMOVED AND REPLACED THE STRINGER IAW SRM 53-21-13.May 17, 2015 · N332NW · Airbus A320211 · Fuselage Main, Longeron/Stringer
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